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High-voltage, high-power, solid-state remote power controllers for aerospace applicationsTwo general types of remote power controller (RPC) that combine the functions of a circuit breaker and a switch were developed for use in direct-current (dc) aerospace systems. Power-switching devices used in these designs are the relatively new gate-turnoff thyristor (GTO) and poweer metal-oxide-semiconductor field-effect transistors (MOSFET). The various RPC's can switch dc voltages to 1200 V and currents to 100 A. Seven different units were constructed and subjected to comprehensive laboratory and thermal vacuum testing. Two of these were dual units that switch both positive and negative voltages simultaneously. The RPC's using MOSFET's have slow turnon and turnoff times to limit voltage spiking from high di/dt. The GTO's have much faster transition times. All RPC's have programmable overload tripout and microsecond tripout for large overloads. The basic circuits developed can be used to build switchgear limited only by the ratings of the switching device used.
Document ID
19850012953
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Sturman, J. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1985
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.60:2437
NASA-TP-2437
E-2359
Report Number: NAS 1.60:2437
Report Number: NASA-TP-2437
Report Number: E-2359
Accession Number
85N21263
Funding Number(s)
PROJECT: RTOP 506-55-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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